View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 55820U 26145.36743345 +.00000000 +00000-0 -33645-3 0 00001
2 55820 87.8948 294.2472 0001755 86.6407 273.4924 13.14502268 08
| Epoch (UTC): | 25 May 2026 08:49:06 |
| Eccentricity: | 0.0001755 |
| inclination: | 87.8948° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2472° |
| argument of perigee: | 86.6407° |
| revolutions per day: | 13.14502268 |
| mean anomaly at epoch: | 273.4924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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